Chapter 7 - Bell 206L4 Maintenance Manual

BHT-206L4-MM-1
5-16. 100-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 1 (CONT)
DATA REFERENCE
Chapter 11

Chapter 71

5-00-00
Page 20 Rev. 13 25 FEB 2011
PROGRESSIVE INSPECTIONS
INSPECTION TASK DESCRIPTION
c. Deformed or cracked skin in the area of the chordwise
weights.
d. Leading edge for erosion, nicks, dents or scratches.
e. Bonded joints of blade skin mating area for suspected
voids or cracks. Pay particular attention in the area of tip block
and doublers.
f. Feathering bearings for looseness and cracks in uniball.
4. Examine the following tail rotor hub and blade assembly
attaching components for condition and security:
a. Spacer
b. Rubber bumper
c. Static stop
d. Nut
e. Balance wheel
ZONE 3 — FORWARD DECK
PLACARDS AND MARKINGS
1. Examine the placards, decals and markings. Make sure
they are readable, correctly applied and in agreement with the
applicable configuration of your helicopter.
AIRFRAME (FORWARD DECK)
1. Open and examine forward fairing for condition and
security.
2. Remove and examine transmission cowling for condition.
3. Examine all fairing and cowling latches and/or fasteners for
condition
4. Examine top deck for condition, leaks and security.
INITIAL
MECH OTHER
ECCN EAR99